Title :
Parametric robustness analysis for Cassini spacecraft using the LMI approach without frequency sweep
Author :
Chiang, Richard Y.
Author_Institution :
Jet Propulsion Lab., California Inst. of Technol., Pasadena, CA, USA
fDate :
29 June-1 July 1994
Abstract :
A generalized Popov multiplier theory enables one to analyze system robustness with mixed real/complex parameters, repeated uncertainties, and multi-dimensional block uncertainties. Using the Cassini spacecraft thrust vector control (TVC) system as a design case study, modern robust control theory has been applied to the real flight project.
Keywords :
aerospace control; attitude control; matrix algebra; robust control; Cassini spacecraft; Cassini spacecraft thrust vector control system; LMI approach; generalized Popov multiplier theory; mixed real/complex parameters; modern robust control theory; multi-dimensional block uncertainties; parametric robustness analysis; repeated uncertainties; Frequency; Fuels; Moon; Robust control; Robust stability; Robustness; Saturn; Space vehicles; Stability analysis; Uncertainty;
Conference_Titel :
American Control Conference, 1994
Print_ISBN :
0-7803-1783-1
DOI :
10.1109/ACC.1994.752252
